DCM[1][2] = cos(pitch) * sin(roll)
DCM[2][0] = sin(heading) * sin(roll) + cos(heading) * sin(pitch) * cos(roll)
DCM[2][1] = -cos(heading) * sin(roll) + sin(heading) * sin(pitch) * cos(roll)
DCM[2][2] = cos(pitch) * cos(roll)
10.11.5
Filter Options Packet
Packet ID
Length
Field #
Bytes
Data
Offset
Type
1
0
u8
2
1
u8
3
2
u8
4
3
u8
5
4
u8
6
5
u8
7
6
u8
8
7
u8
9
8
Table 98: Filter options packet
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Filter Options Packet
Size
1
1
Vehicle type, see section 10.11.5.1
1
Internal GNSS enabled (boolean)
1
1
Atmospheric altitude enabled (boolean)
1
Velocity heading enabled (boolean)
1
Reversing detection enabled (boolean)
1
Motion analysis enabled (boolean)
9
GNSS Compass Reference Manual
Page 78 of 85
Version 1.1
13/01/2021
186
17
Description
Permanent
Reserved (set to zero)
Reserved (set to zero)
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